SAE ARP5414A
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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Aircraft Lightning Zone
Hardcopy , PDF
10-12-2018
English
28-09-2012
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1 SCOPE
2 REFERENCES
3 BACKGROUND
4 AIRCRAFT LIGHTNING INTERACTION
5 ZONE DEFINITIONS
6 WAVEFORM APPLICABILITY
7 ZONE LOCATION PROCESS
8 INITIAL LEADER ATTACHMENT LOCATION METHODS
9 OTHER ZONING CONSIDERATIONS
10 PROTECTION CONSIDERATIONS
11 NOTES
Defines lightning strike zones and provides guidelines for locating them on particular aircraft, together with examples.
| DocumentType |
Standard
|
| Pages |
33
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
This SAE Aerospace Recommended Practice (ARP) defines lightning strike zones and provides guidelines for locating them on particular aircraft, together with examples. The zone definitions and location guidelines described herein are applicable to Parts 23, 25, 27, and 29 aircraft. The zone location guidelines and examples are representative of in-flight lightning exposures.
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| SAE ARP5412B | Aircraft Lightning Environment and Related Test Waveforms |
| MIL-STD-461 Revision G:2015 | REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT |
| SAE AIR5691A | Guidance for the Design and Installation of Fuel Quantity Indicating Systems |
| FAA AC 25-11 : 2014 | ELECTRONIC FLIGHT DISPLAYS |
| NASA STD 4003 : 2013 | ELECTRICAL BONDING FOR NASA LAUNCH VEHICLES, SPACECRAFT, PAYLOADS, AND FLIGHT EQUIPMENT |
| MIL-STD-464 Revision C:2010 | ELECTROMAGNETIC ENVIRONMENTAL EFFECTS REQUIREMENTS FOR SYSTEMS |
| SAE AIR6185 | Aerospace - Lightning Effects on Hydraulic Transport Elements on Aircraft |
| SAE ARP5416A | Aircraft Lightning Test Methods |
| SAE AS8017D | Minimum Performance Standard for Anticollision Light Systems |
| NASA JSC 08080-2 : 2015 | JSC DESIGN AND PROCEDURAL STANDARDS |
| SAE AIR 6464 : 2013 | EUROCAE/SAE WG80/AE-7AFC HYDROGEN FUEL CELLS AIRCRAFT FUEL CELL SAFETY GUIDELINES |
| FAA AC 20-136 : 2011 | AIRCRAFT ELECTRICAL AND ELECTRONIC SYSTEM LIGHTNING PROTECTION |
| SAE AIR 5774 : 2012 | COMPOSITE FUEL TANKS, FUEL SYSTEM DESIGN CONSIDERATIONS |
| SAE ARP5415A | User\'s Manual for Certification of Aircraft Electrical/Electronic Systems for the Indirect Effects of Lightning |
| SAE AIR 4004 : 2015 | GUIDE FOR INSTALLATION OF ELECTRICAL WIRE AND CABLE ON AIRCRAFT LANDING GEAR |
| FAA AC 27-1 : 2008 | CERTIFICATION OF NORMAL CATEGORY ROTORCRAFT |
| FAA AC 21-16 : 2011 | RTCA DOCUMENT DO-160 VERSIONS D, E, F, AND G, "ENVIRONMENTAL CONDITIONS AND TEST PROCEDURES FOR AIRBORNE EQUIPMENT" |
| FAA AC 20-53 : 2006 | PROTECTION OF AIRCRAFT FUEL SYSTEMS AGAINST FUEL VAPOR IGNITION CAUSED BY LIGHTNING |
| FAA AC 20-136 : 2011 | AIRCRAFT ELECTRICAL AND ELECTRONIC SYSTEM LIGHTNING PROTECTION |
| SAE ARP 5415 : 2002 | USER'S MANUAL FOR CERTIFICATION OF AIRCRAFT ELECTRICAL/ELECTRONIC SYSTEMS FOR THE INDIRECT EFFECTS OF LIGHTNING |
| FAA AC 23.1309-1 : 2011 | SYSTEM SAFETY ANALYSIS AND ASSESSMENT FOR PART 23 AIRPLANES |
| SAE ARP5416A | Aircraft Lightning Test Methods |
| FAA AC 29-2 : 2008 | CERTIFICATION OF TRANSPORT CATEGORY ROTORCRAFT |
| SAE ARP5412B | Aircraft Lightning Environment and Related Test Waveforms |
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